What was found
DURING INSPECTION, TWO GOUGES WERE FOUND ON NR 1 ENGINE STRUT RIGHT SKIN PANEL NEAR AN ACCESS DOOR CUTOUT. MAXIMUM DEPTH OF BLEND OUT REQUIRED TO COMPLETELY REMOVE DAMAGE WAS 0.035 INCH. REPAIRED AREA IAW REA B654-46243MR.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING INSPECTION, TWO GOUGES WERE FOUND ON NR 1 ENGINE STRUT RIGHT SKIN PANEL NEAR AN ACCESS DOOR CUTOUT. MAXIMUM DEPTH OF BLEND OUT REQUIRED TO COMPLETELY REMOVE DAMAGE WAS 0.035 INCH. REPAIRED AREA IAW REA B654-46243MR.